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136                   Finite Element Modeling and Simulation with ANSYS Workbench



                   TABLE 4.1
                   FEA Stress Results
                   Elem. Type        No. of Elem.        Total DOFs        Max. σ (psi)
                   Q4                    506                1102             312.42
                   Q4                   3352                7014             322.64
                   Q4                  31,349              64,106            322.38
                   ...                   ...                 ...               ...
                   T6                   1518                6254             320.18
                   T6                   2562               10,494            321.23
                   T6                  24,516             100,702            322.24
                   ...                  ...                  ...               ...
                   Q8                    501                3188             320.58
                   Q8                   2167               13,376            321.70
                   Q8                  14,333              88,636            322.24






                  The stress calculations with several meshes are listed in  Table 4.1, along with the
                   number of elements and DOFs used.
                  The converged results are obtained with all three types of elements with the differ-
                 ences in the maximum stress values less than 0.05%. However, Q8 and T6 elements are
                 more efficient and converge much faster than the Q4 elements which are a linear rep-
                 resentation and cannot model curved boundaries accurately. If the required accuracy
                 is set at 1%, then the mesh with 501 Q8 elements should be sufficient. Note also that
                 we need to check the deformed shape of the plate for each model to make sure the BCs
                 are applied correctly. Fewer elements should be enough to achieve the same accuracy
                 with a better or “smarter” mesh (mapped mesh). We will redo this example in the next
                 chapter employing the symmetry features of the problem.



            4.4.8  General Comments on the 2-D Elements
               a. Know the attributes of each type of elements:
                 T3 and Q4:  Linear displacement, constant strain and stress
                 T6 and Q8:  Quadratic displacement, linear strain and stress
               b. Choose the right type of elements for a given problem:
                 When in doubt, use higher order elements (T6 or Q8) or a finer mesh.
               c. Avoid elements with large aspect ratios and corner angles (Figure 4.17):
                 Aspect ratio = L max /L min  where L max  and L min  are the largest and smallest character-
                 istic lengths of an element, respectively.
              d. Make sure the elements are connected properly:
                 Do not leave unintended gaps or free elements in FE models (Figure 4.18).
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